Direct numerical simulation of acoustic reduction using serrated trailing-edge on an isolated airfoil
Work
Year: 2014
Type: article
Institution Université de Sherbrooke
Cites: 25
Cited by: 42
Related to: 10
FWCI: 3.873
Citation percentile (by year/subfield): 96.74
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed